Journal of Thermal Engineering
metadata only
Aerodynamic Study of Slotted Flap for NACA 24012 Airfoil by Dynamic Mesh Techniques and Visualization Flow
Slotted flap is one of high lift devices. It considered as a moving part of the airfoil which is used as a control instrument in a form of elevator, rudders and ailerons. The main focus of work is to investigate the effect of flap chord, gap and overlap on aerodynamic characteristic of NACA 24012 air
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- Aeroelasticity of Insect-inspired Flapping Wings with Anisotropic Rigidity#142471
- Structural aspects of suction wings#491439
- Separated flows over swept wings across transitional Reynolds numbers#1143333
- The Effect of Blowing Direction on Heat Sink Performance by Thermal Imaging#932438
- ACSS Approach on Dysphagia#830933
Record · ID 932613
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive